粘流運動方程 的英文怎麼說

中文拼音 [niánliúyùndòngfāngchéng]
粘流運動方程 英文
viscous equation of motion
  • : 粘動詞(粘附) glue; stick; paste; adhere to; bond
  • : Ⅰ動1 (液體移動; 流動) flow 2 (移動不定) drift; move; wander 3 (流傳; 傳播) spread 4 (向壞...
  • : Ⅰ動詞1 (物體位置不斷變化) move; revolve 2 (搬運; 運輸) carry; transport 3 (運用) use; wield...
  • : Ⅰ名詞1 (方形; 方體) square 2 [數學] (乘方) involution; power 3 (方向) direction 4 (方面) ...
  • : 名詞1 (規章; 法式) rule; regulation 2 (進度; 程序) order; procedure 3 (路途; 一段路) journe...
  • 運動 : 運動[舊時用語] arrange things or get things done through pull
  1. The way to get ko was given in this paper. by this way, the turbulence control equations were constructed from reynold equations with static pressure supposition and boussinesq ' s turbulence viscidity coefficient supposition and the salinity transportation equations, which are representative of the matter transportation equations, are given. the integrated deduction and corresponding boundary conditions are also given

    根據上述思想,從雷諾出發,採用靜壓假定和包辛內斯克的紊性系數假說,建立了新坐標系中的紊控制組,同時給出了對物質輸具有代表性的鹽度輸、相應的邊界條件及完整的推導過
  2. In this paper, some characteristics of flow movement and sediment transport are analyzed by using the flume experiment data. the cross section of compound channel can be divided into four regions : the undisturbed region in main channel, the interactive region between channel and plain, the undisturbed region in flood plain and the boundary region. in the undisturbed regions, the distribution of longitudinal velocity along the depth has the feature of lograithmic. whereas, in the interactive region, the longitudinal velocity does not obey the logarithmic distribution law, but it can expressed as a revised logarithmic function by using a wake function. on the basis of the kinematic equation the velocity distribution of transverse velocity is obtained. in the boundary region, the longitudinal velocity obeys the law of parabolic distribution. furthermore, according to the simplified diffusion equation, the transverse distribution of sediment concentration in the interactive region is deduced. the analysis is in good agreement with the measured data

    本文根據漫灘水特點,將漫灘水的復式斷面分為主槽平衡區、灘槽交互區、灘地平衡區及邊壁區等4個區,並給出了各區寬度的經驗公式.根據灘槽交互區垂線速分佈的變化特點,提出了附加尾函數的對數速分佈公式.在簡化水和泥沙擴散的基礎上,對灘槽交互區內垂線平均速及含沙量沿橫向分佈進行了理論分析,提出了反映灘槽水量交換強度的橫向渦量性系數及橫向擴散系數的表達式,得到了漫灘水垂線平均速及含沙量沿橫向分佈的解析解,並與實測資料吻合較好
  3. As is known to all, navier - stokes equations are fundamentally important in describing the motion for viscous incompressible fluids. for a long time, these equations have been deeply investigated by a lot of scientific workers, including many famous mathematicians

    作為描述性不可壓縮規律的基本, navier - stokes長期以來得到包括許多著名數學家在內的眾多科學工作者的廣泛關注。
  4. The total pressure is subdivided into the hydrostatic and residual hydrodynamic components. k - e turbulent flows model, non - staggered curvilinear grids, momentum interpolation, simplec and simpler algorithms are used to solve the basic equations

    壓力項分解為靜水壓力和水壓力,紊性系數由k紊模型求解,非交錯網格減化離散,降低插值算。
  5. For the present two les models, adopting the subgrid eddy viscosity concept and introducing the transport equation of turbulence energy k, the subgrid scale turbulence is parameterized by the turbulence energy k and the length scale of turbulence / ( k - 1 model ). in addition, vegetation is considered as an internal source of resistant force and turbulence energy

    在應用大渦模擬法求解數值計算模型控制時,亞網格雷諾應力項沿用了亞網格渦性系數思路,引入亞網格紊能k的輸,建立了關于亞網格紊能k和紊特徵長度l的k - l模型求解。
  6. Then the steady and unsteady subsonic, transonic and supersonic viscous flows around airfoil and some aircraft are numerically simulated. the 3 - dimensional unsteady navier - stokes equations are solved using the implicit lu - nnd algorithm, with baldwin - lomax turbulent model. on the basis of simulating unsteady viscous flow, coupling the structure dynamics equations, the problems of static aeroelasticity and flutter are investigated for wings and elevator

    在模擬非定常性繞的基礎上,與顫振相耦合,分別對機翼和全機固耦合現象中顫振問題進行了研究,準確求解跨音速顫振臨界速度,分析機翼和全機的從亞音速到超音速范圍的顫振規律,並研究分析了機翼飛行迎角變化對顫振速度的影響。
  7. On three - dimensional numerical solution of incompressible viscous flow by osfem abstract an algorithm for solution of three - dimensional navier - stokes equations for incompressible viscous flow is developed. a decoupled algorithm based on the operator - splitting technique is applied

    由於三維的復雜性,例如邊界的選取、控制條件的給定以及混合算元高精度數值解法等,都值得探討和研究。
  8. The navier - stokes equation is discretized in the moving - grid system. by adopting the explicit four - stage runge - kutta jameson finite volume scheme, and under the sustainment of acceleration algorithms such as dual - time stepping method, the multi - grid strategy and implicit smoothing of the residuals, a two dimensional unsteady viscous flow in vibrating cascades is simulated

    本文在網格體系中離散n - s,應用runge - kutta四步顯式的jameson有限體積格式,並在雙時間法、多重網格法及殘差光順等加速演算法的支持下,計算了二維振葉柵非定常場。
  9. The moving grid of type c - h for wing are generated by an algebraic procedure. the steady and unsteady transonic ( and subsonic ) viscous flows around wing are numerically simulated. the 3 - dimensional time - averaged compressible navier - stokes equations with b - l or j - k turbulent models are solved by the implicit lu - n7nd algorithm

    用代數法生成機翼的c - h型網格,從三維非定常n - s組出發,利用lu - nnd有限差分格式和b - l或j - k湍模型建立了一種數值模擬三維機翼的亞、跨、超音速定常及非定常性繞法和序。
  10. Because the equation of shallow water and the equation of inviscid compressible flow have completely similar mathematical forms, a lot of mathematical concepts and methods - including the numerical simulation method of aerodynamics can be used in the research of the shallow wave

    由於數學上淺水長波與可壓縮氣體的無類似,可以把淺水長波比擬成可壓縮氣體無,將空氣力學中所得到的許多數學概念和法(包括數值法)直接應用於淺水長波的
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